MATLAB AEROSPACE TOOLBOX RELEASE NOTE Manuale Utente Pagina 20

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R2014a
3-2
Blocks to convert between latitude, longitude, altitude and Earth-centered
inertial coordinates
The LLA to ECI Position block in the Utilities/Axes Transformations sublibrary converts
geodetic latitude, longitude, altitude (LLA) coordinates to Earth-centered inertial (ECI)
position coordinates, based on the specified reduction method and Universal Coordinated
Time (UTC), for the specified time and geophysical data.
The ECI Position to LLA block converts Earth-centered inertial (ECI) position
coordinates to geodetic latitude, longitude, altitude (LLA) coordinates, based on the
specified reduction method and Universal Coordinated Time (UTC), for the specified time
and geophysical data.
Flight simulator interface block support for FlightGear Version 2.12
These blocks support FlightGear v2.12:
FlightGear Preconfigured 6DoF Animation
Generate Run Script
Pack net_fdm Packet for FlightGear
Receive net_ctrl Packet from FlightGear
Unpack net_ctrl Packet from FlightGear
For more information on working with FlightGear, see Flight Simulator Interfaces.
Equations of Motion 3DOF and 6DOF handle large mass changes
The following 3DOF and 6DOF blocks have been extended to handle large mass
changes over time:
Custom Variable Mass 3DOF (Body Axes)
Custom Variable Mass 3DOF (Wind Axes)
Simple Variable Mass 3DOF (Body Axes)
Simple Variable Mass 3DOF (Wind Axes)
Custom Variable Mass 6DOF (Euler Angles)
Custom Variable Mass 6DOF (Quaternion)
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